Estimating Performance Capabilities of Boost Rockets (I and II)

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Garabedian, P. and R.P. Ten Dyke. Estimating Performance Capabilities of Boost Rockets. TRW Space Technology Labs, Los Angeles, 10 September 1959. 11.5 x 8.5 , ii, 39pp. __+__ NO copies located in WorldCat/OCL__+__ Abstract :"The results are reported on a parametric study of boost rockets. The term boost rocket includes rockets launched from the surface of the earth for the purpose of achieving near-orbital or greater velocities. The parameters studied are divided into two categories: vehicle design parameters and trajectory parameters. Vehicle design parameters describe the physical rocket and include such quantities as weights, thrusts, propellant flow rates, drag coefficients, and the like. Trajectory parameters include such quantities as impact range, apogee altitude, and burnout velocity. --from Defense Technical Information Website __+__ Bound with: Estimating Performance of Boost Rockets II. Same publisher and format. 3Pp plus 5 leaves of data. Stapled to the front inside wrapper. N° de ref. del artículo ABE-1569123222580

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